BACKGROUND OF THE INVENTION
[0001] This invention relates generally to a rotary fluid power transmission in the form
of a pump or motor, and more particularly concerns a variable displacement gerotor
pump.
[0002] It is well known that conventional gerotor pumps are positive displacement pumps
that are self-priming, lightweight and require no valves for operation. Gerotor pumps
have long been used to pump impure fluids and are durable, long-wearing devices.
[0003] and A conventional gerotor pump includes two pumping elements, referred to herein
as an inner rotor and an outer rotor. The inner rotor is generally secured to a drive
shaft and always has one less tooth than the outer rotor. As the inner rotor is rotated
on the drive shaft, it advances one tooth space per revolution relative to the outer
rotor. The outer rotor is rotatably retained in a housing, eccentric to the inner
rotor, and meshing with the inner rotor on one side. As the inner and outer rotors
turn from their meshing point the space between the teeth of the inner and outer rotors
gradually increases in size through the first 180° rotation of the inner rotor, creating
a partial vacuum therebetween. The fluid to be pumped is drawn from an inlet port
into the enlarging space. During the last half of the revolution cycle, the space
between the inner and outer rotors decreases in size as the teeth mesh and the fluid
is forced from the space. As the space between the inner and outer rotors decreases
in volume, it is open to an outlet port. The inlet and outlet ports are isolated from
each other by the housing and the inner and outer rotors.
[0004] Such gerotor pumps are constant, displacement pumps which yield a predetermined displacement
per revolution. In many applications. this is a desirable feature, however, in some
applications it is desirable to change displacement without altering the speed of
rotation of the drive shaft with a variable displacement pump.
[0005] While the advantages of a variable displacement pump are well known, prior art devices
that have attempted to provide such a pump tend to be complex structures that are
difficult to manufacture and subject to leakage or even failure. The degree of variability
realizable in prior art gerotor pumps is severely limited. In particular, prior art
variable displacement gerotor pumps are complex and are not generally as effective
as other types of variable displacement pumps.
[0006] Conventional variable delivery gerotor pumps typically use a bypass to divert a portion
of the fluid pumped from the fluid output channel of the pump to the reservoir or
intake of the pump. The fluid may be either moved through a bypass channel or will
flow internally from the outlet side of the pump to the inlet side. When variability
is obtained by means of bypass, there is little power savings since the power requirement
of the pump will remain the same even as delivery is reduced. If the fluid is permitted
to flow internally from the outlet side of the pump to the inlet side, power is converted
into heat which will build up in the fluid and pump, and will result in reduced service
life of the fluid and pump. Many bypass systems also cause cavitation.
[0007] Another type of prior art mechanism used to create a variable delivery gerotor pump
did so by restricting the outlet port of the pump. In this approach to the problem,
restrictions in the outlet port result in excessive noise and vibration in the pump.
Restricting the outlet causes fluid to be trapped in the pump which contravenes the
traditional principles of fluid power engineering. Excessive noise and vibration in
such devices is unacceptable in many applications and frequently will result in accelerated
wear.
[0008] These and other disadvantages and limitations have been overcome in the present invention.
While the simple and effective displacement control achieved by the present invention
is best applied to gerotor pumps, it can also be applied to gear pumps, vane pumps,
and other types of fluid rotary power transmissions including fluid rotary motors.
SUMMARY OF THE INVENTION
[0009] The present invention relates to a variable displacement gerotor pump which is simply
constructed for dependability, durability, and ease of manufacture. Durability of
the displacement control mechanism enhances the dependability of pumps made in accordance
with the present invention. The component parts of the pump made in accordance with
the present invention are not complex so they may be machined to close tolerances,
thereby limiting the need for seals in many instances.
[0010] The variable displacement gerotor pump of the present invention achieves substantial
power savings because the power requirement of the pump is reduced proportionately
to the reduction in displacement required. The present invention provides variable
displacement without bypassing excess fluid from the outlet port back to the inlet
port or reservoir and prevents cross flow from the outlet side of the pump to the
inlet side. Variable displacement is achieved without restricting the inlet flow or
outflow of fluid from the pump.
[0011] The present invention is a pump of general application which is well suited for retrofitting
into existing systems to provide additional pumping capacity.
[0012] The variable displacement gerotor pump of the present invention is a positive displacement
pump which is self priming in its mimimum flow position. Most other types of variable
displacement pumps such as a vane pump do not prime in their minimum 'flow positions
which complicates start up of a machine using such pumps.
[0013] - The variable displacement gerotor pump of the present invention is capable of providing
a wide range of displacement volume per revolution ratios. Control of displacement
may be provided by either a simple manual control or a hydraulic control system.
[0014] The manual pump control uses a lever which is connected to a positionable control
device within the pump which simultaneously changes the effective size of the inlet
and outlet ports without restriction of fluid flow and rotates the eccentric axis
of the outer rotor about the central axis of the inner rotor to change the volume
of fluid transferred by the pump from the inlet port to the outlet port.
[0015] The hydraulically controlled embodiment of the present invention comprises a hydraulic
fluid channel formed in the positionable control device which includes fluid reaction
members effective to rotate the positionable control device in one direction when
fluid is injected into the channel. A biasing member is preferably provided in the
channel to rotate the positionable control device in the opposite direction when fluid
is withdrawn from the channel.
[0016] In one embodiment an automatic displacement adjusting pump is provided wherein the
outlet port of the variable displacement gerotor pump is connected by a control fluid
port to the channel in the positionable control device, so that an increase in demand
on the pump results in a reduction in fluid pressure within the channel. Reduction
of the fluid pressure in the channel causes the positionable control device to rotate
to an increased flow position. Conversely, when the hydraulic system demand is reduced,
the pressure in the outlet port increases. Increase in pressure is communicated to
the channel through the control, fluid port to shift the positionable control device
to a reduced flow position.
[0017] According to the present invention, a pump is provided which has a housing including
a cylindrical bore with a fluid inlet and a fluid outlet opening into the bore. A
pump mechanism is rotatably nested within a positionable control device which is in
turn nested within the cylindrical bore of the housing. The pump mechanism is nested
within an eccentric inner diameter formed in the positionable control device. The
pump mechanism includes an outer controlled member rotatably nested within the positionable
control device and a power driven inner control member concentric with the cylindrical
bore and eccentric to the outer controlled member. The inner control member, or inner
rotor, engages the outer controlled member, or outer rotor, to provide a fluid pumping
action, as previously described, between the fluid inlet and fluid outlet. The eccentric
position of the outer controlled member relative to the inner control member may be
varied by rotating the positionable control device to change the quantity of fluid
pumped per revolution of the control members.
[0018] In another embodiment of the present invention, a variable displacement gerotor pump
is provided in a pump housing having a cylindrical bore with a port plate at one end
and a removable cover on the opposite end. The port plate includes a fluid intake
port and a fluid outlet port. The inlet and outlet ports are separated at one circumferential
location by a commutator which includes an annular portion and a lobe -fixedly located
on the surface of the port plate between the fluid inlet and outlet ports. A positionable
control device, adapted to nest within the cylindrical bore, on the surface of the
port plate, is arcuately shiftable relative to the commutator and has a lobe extending
toward the commutator for providing a rotatable seal between the other end of the
fluid inlet and outlet ports. A device for adjusting the positionable control device
is provided to shift the pump between a maximum flow position and a minimum flow position.
In this embodiment, the gerotor pump elements are positioned within the eccentric
bore of the positionable control device so that the relative eccentricity of the inner
and outer rotors is shifted when the positionable control device is rotated. In this
way, the effective size of the outlet port and the location of the eccentric axis
are simultaneously shifted by the positionable control device.
[0019] In a hydraulically controlled embodiment of the present invention, the positionable
control device includes a fluid reaction chamber formed on the side of the positionable
control device adjacent the housing. A rotable reaction member is attached to the
positionable control device and a stationary reaction member is attached to the housing.
A channel or port is formed through the housing to supply and withdraw fluid into
and out of the fluid reaction chamber to cause the positionable control device to
rotate relative to the housing.
[0020] In automatically controlled embodiment of the present invention, a channel interconnects
the fluid outlet of the pump to the fluid reaction chamber of the positionable control
device to create an automatically controlled variable displacement gerotor pump.
BRIEF DESCRIPTION OF THE DRAWINGS
[0021]
Figure 1 is an exploded perspective view of a manually controlled variable displacement
gerotor pump according to the present invention.
Figure 2 is a sectional view of the present invention.
Figure 3 is a fragmentary end view of the present invention with the positionable
control device in the minimum flow position.
Figure 4 is a fragmentary end view of the present invention with the positionable
control device in the maximum flow position.
Figure 5 is a plan view of the positionable control device of the present invention.
Figure 6 is a cross-sectional view of the positionable control device taken along
the line 6-6 in Figure 5.
Figure 7 is a plan view of the commutator of the present invention.
Figure 8 is a cross-sectional view of the commutator taken along the line 8-8 in Figure
7.
Figure 9 is a plan view of the pump housing of the present invention.
Figure 10 is a cross-sectional view of the pump housing taken along the line 10-10
in Figure 9.
Figure 11 is a fragmentary cross-sectional end view of a hydraulically controlled
variable displacement pump made in accordance with a preferred embodiment of the present
invention.
Figure 12 is a cross-sectional view of the hydraulically controlled variable displacement
pump shown in Figure 11 taken along the line 12-12.
DETAILED DESCRIPTION
[0022] Referring now to the drawings, the variable displacement pump 10 includes a housing
12 having a centrally located cylindrical bore 13 extending partially through the
housing 12. The end of the cylindrical bore comprises a port plate 14 through which
hydraulic fluids are pumped. The pump-10 is powered by means of a drive shaft 15 which
is centrally mounted within the cylindrical bore 13. A commutator 16 is stationarily
mounted on the port plate 14 to encircle the end of the cylindrical bore 13. A positionable
control device, or variator 17, is nested within the cylindrical bore 13 of the housing
12. The variator 17 includes a concentric inner surface 18 axially adjacent the port
plate 14 and an eccentric inner surface, or eccentric bore 19, axially adjacent the
concentric inner surface 18. A gerotor pump mechanism 20 is disposed within the eccentric
bore 19 and comprises an outer rotor 21 and an inner rotor 22. The'housing 12 is enclosed
by a cover, or end plate 24, which holds the commutator 16, variator 17 and gerotor
pump mechanism 20 together within the housing 12 in their operative relationship on
the drive shaft 15.
[0023] Referring now to Figures 1, 2, 9 and 10, the housing 12 is shown to include an inlet
port 26 which is in communication with a reservoir or source of fluid (not shown).
The inlet port 26 is an arcuate opening formed through the port plate 14. The outlet
port 27 is an opening formed in the port plate 14 spaced from the inlet port 26. The
outlet port 27 is preferably smaller than the inlet port 26. The central bore 28 is
formed in the center of the port plate 14 and extends through the housing 12. A ball
bearing 29 is located in the housing to journal the drive shaft 15 for rotation in
the central bore 28. The housing 12 includes a flange 30 at the open end of the cylindrical
bore 13 for securing the cover plate 24 to the housing 12.
[0024] The cover plate 24 is provided tu enclose the cylindrical bore 13 of the housing
12. The cover plate 24 is formed with an axial boss 32 to reinforce the cover plate
24 adjacent the bore 33 and to retain a bearing 34 which journals the drive shaft
15. The cover plate 24 is detachably secured to the flange 30 of the housing 12 by
means of a plurality of bolts 35.
[0025] The commutator 16 is provided to block fluid flow from the inlet port 26 to the outlet
port 27. Referring now to Figures 1, 2, 7 and 8, the commutator 16 includes an annular
portion 37 having a bore 38 for encircling the drive shaft 15 and is located annularly
adjacent to the port plate 14. A first lobe, or protrusion 39, extends radially outward
from the annular portion 37 and includes a convex surface 40 at its radially outer
end. The commutator 16 is held in place on the port plate 14 by means of a dowel pin
41 extending from the first lobe 39 into a hole 42 formed in the port plate 14 between
the inlet port 26 and outlet port 27. The commutator 16 may include a cylindrical
sleeve 44 protruding from the side of the commutator 16 and into an annular groove
45 formed in the port plate 14 about the periphery of the central bore 28. The dowel
pin 41 and sleeve 44 being effective to hold the commutator 16 in place on the port
plate 14.
[0026] The variator, or positionable control device 17, as shown in Figures 1, 2, 5 and
6, is a cylindrical member having a concentric inner surface 18 which is approximately
equal in thickness axially to the commutator 16. The variator 17 includes a second
lobe or protrusion 46 extending radially inwardly from the concentric surface 18 to
contact the commutator 16. The second lobe 46 terminates in a concave end 47 that
is machined to the same radius as the annular portion 37 to form a close tolerance
fit therewith. The variator 17 is assembled into the housing 12 to be arcuately shiftable
so that the second lobe 46 may move toward and away from the first lobe 39. The convex
surface 40 of the first lobe 39 has the same radius as the concentric inner surface
18 of the variator 17 to form a seal therebetween.
[0027] Referring now to Figures 3 and 4, an arcuate inlet groove 48 is formed on the inlet
port 26 side of the first and second lobes 39 and 46, and an arcuate outlet groove
49 is formed on the outlet port 27 side of the first and second lobes 39 and 46. The
size of the arcuate inlet and outlet grooves 48 and 49 is variable depending upon
the position of the variator 17. When the second lobe 46 is moved enlarging one of
the arcuate grooves, the other arcuate groove is reduced in size commensurately. The
arcuate outlet groove 49 may be reduced in size until it is substantially equal to
the size of the outlet port 27, as when the pump is in the minimum flow position shown
in Figure 3. The arcuate outlet groove 49 may be enlarged until it is equal to the
size of the inlet groove 48, as when the pump is in the maximum flow position shown
in Figure 4. A stop may be provided , as will be described subsequently, to prevent
movement of the second lobe past the maximum flow position.
[0028] .The central axis of the drive shaft 15 and the concentric inner surface 18 is shown
on Figures 3, 4, 5, and 6 as axis "C". The central axis of the eccentric inner surface
19 of the variator 17 is indicated by the letter "E". The eccentric axis "E" is located
on the opposite side of the central axis "C" from the second lobe 46. Hence, the second
lobe 46 is located on the variator 17 where the concentric inner surface,18 and eccentric
surface 19 are closest together. The inner and outer rotors 22 and 21 are held together
by the variator adjacent the second lobe 46 in a closed mesh relationship, to form
a closed mesh area 62, which is also referred to as the-closed mesh crossover. The
closed mesh area 62 of the rotors and second lobe 46 act to block fluid flow from
the arcuate outlet groove 49 to the arcuate inlet groove 48.
[0029] Conversely, an open mesh area 63, or crossover point, is formed between the teeth
of inner and outer rotors 22 and 21 where the inlet groove 48 and outlet groove 49
are separated by the first lobe 39 of the commutator 16. The open mesh crossover area
63 is the point at which fluid which has been drawn into the space between the inner
and outer rotors 22 and 21 is transferred to the outlet groove 49 and then to the
outlet port 27. The first lobe 39 is sized to prevent cross flow from the outlet groove
49 to the inlet groove 48 as the gerotor pump mechanism 20 is rotated relative to
the lobe 39.
[0030] The present invention achieves variable displacement by repositioning the eccentric
axis "E" of the outer rotor 21 relative to the axis "C" of the inner rotor 22. The
volume of the space 50 at the open mesh crossover 63 is varied by changing the position
of the variator 17 which rotates the second lobe 46 relative to the first lobe 39
while keeping the inlet and outlet grooves 48 and 49 separate. The volume of the space
50 is changed from a minimum, as shown in Figure 3, to a maximum, as shown in Figure
4.
[0031] In the manually shifted embodiment of the present invention, the position of the
variator 17 is changed by moving a handle 51, shown in Figures l and 2. The handle
51 engages, a dowel pin 52 which is secured to the variator and extends through an
arcuate slot 53 in the cover plate 24. The ends of the arcuate slot 53 act as stops
to limit the range of rotation of the variator 17 to the space between the inlet and
outlet ports 26 and 27.
[0032] The outer rotor 21 of the gerotor pump mechanism 20 is nested within the eccentric
inner surface 19 of the variator 17. The outer rotor 21 has a cylindrical outer surace
54 and an inner surface 55 haying a plurality of convex arcuate gear teeth 56..
[0033] - The inner rotor 22 is attached to the drive shaft 15 to be concentric therewith
while being eccentric to the inner surface 55 of the outer rotor 21. The outer surface
58 of the inner rotor 22 includes a plurality of concave arcuate gear teeth 59 that
are adapted to engage the convex gear teeth 56 of the outer rotor 21. As in conventional
gerotor mechanisms the inner rotor has one less tooth than the outer rotor 21. A pumping
action is created by the increasing and decreasing size of the clearance space between
the inner and outer rotor 22 and 21 with the inlet and outlet ports 26 and 27 being
isolated from one another. The inner rotor includes a concentric bore 60 having a
keyway 61 by which the inner rotor is secured to the drive shaft 15, as shown in Figure
2. A key 64 interconnects the drive shaft 15 to the inner rotor 22 so that the inner
rotor rotates with the drive shaft 15.
[0034] In the disclosed embodiment, the entire gerotor pump assembly is mounted by means
of a mounting bracket 66 which holds the pump stationary as the drive shaft 15 is
rotated by a power source (not shown).
[0035] As with a conventional gerotor pump mechanism, the inner rotor 22 is rotated by the
drive shaft 15 which in turn causes the outer rotor 21 to be rotated by the action
of the gear teeth 56 and 59. Rotation of the outer rotor 21 is resisted by a frictional
force developed between the cylindrical surface 54 and the eccentric inner surface
19 of the variator 17. If the inner and outer rotors 22 and 21 rotate in the clockwise
direction, as viewed in Figure 3, the frictional force between the cylindrical surface
54 and the eccentric inner surface 19 will tend to bias the variator 17 for rotation
in the clockwise direction. Rotation of the variator 17 within the housing 12 is resisted
by friction between the housing 12 and variator 17. If it is desirable to reduce the
frictional force resisting rotation of the variator 17, roller bearings may be mounted
between the housing and the variator to facilitate rotation of the variator relative
to the housing. Roller bearings 68 are shown in Figures 2 through 4 to illustrate
this variation.
[0036] Referring now to Figures 11 and 12, an automatically adjusted variable displacement
pump 70 is shown which includes a unique displacement adjustment mechanism. The automatically
adjusted pump 70 permits the displacement of the pump to be adjusted according to
the fluid demand of a hydraulic system. When the demand for hydraulic fluid increases,
the reduction in pressure causes the pump output to be adjusted to provide additional
displacement to compensate for the increase in demand. Conversely, when demand is
reduced in the hydraulic system, the automatically adjusting variable displacement
pump reduces the delivery of fluid through the pump.
[0037] The automatically adjusted variable displacement pump 70 includes a housing 71 which
has a cylindrical bore 72 with a closed end 73. The internal elements of the variable
displacement pump shown in Figures 11 and 12 are placed in the housing 71 in the inverse
position as was described for the manual embodiment of Figures 1 through 10.
[0038] The commutator 74 has a dowel pin 75 extending from one side into cover plate 76,
which also acts as the port plate of the pump 70. The outlet port 77 extends through
the port plate 70, as shown in Figure 12, and includes means for receiving a hydraulic
fitting. The cover plate includes an axial boss 78 which retains a needle bearing
set 79 for journaling one end of the shaft 80 for rotation.
[0039] The internal portions of the variator 82 and the gerotor 84 may be shaped the same
as the manual embodiment previously described. The interaction of the variator 82,
commutator 74, and gerotor 84 are preferably identical to the manual embodiment previously
described and will not be repeated.
[0040] The variator 82 includes an annular groove, or chamber 92, formed in its outer cylindrical
surface. A stationary reaction member 93 is positioned in the annular groove 92 and
secured to the housing 71 by means of a screw or other fastener 94 as shown in Figure
11. A shiftable reaction member 95 also located in the annular groove 92 and is attached
to the variator 82. The stationary and shiftable reaction members 93 and 95 are interconnected
by a spring, or biasing member 96, which is also preferably located in the annular
groove 92.
[0041] The housing 71 includes a control fluid port 98 opening into the cylindrical bore
72 on the opposite side of the gerotor from the outlet port to communicate pressure
changes in the outlet port 77 to the annular groove 92. The control fluid port 98
opens into the annular groove 92 between the stationary and shiftable reaction members
93 and 95 so that an increase in fluid pressure in the outlet port 77 causes the fluid
pressure in the annular groove 92 to increase, forcing the shiftable reaction member
95 to move counterclockwise toward the position shown in phantom lines in Figure 11.
Movement of the shiftable reaction member causes the variator 82 to rotate toward
the minimum flow position thereby causing the displacement of the pump to be reduced.
[0042] Movement of the variator 17 may be stopped by a ball stop 97 which is shown disposed
in the wall of =the housing 71 to contact the reaction member 95. Alternatively, a
ball stop could be located on the commutator 74 adjacent the outlet port 77 to engage
the lobe of the variator to prevent it from covering the outlet port 77. In some applications
it is anticipated that the lobe of the variator would be permitted to move over the
outlet port 77.
[0043] . Movement of the shiftable reaction member 95 is opposed by the spring 96, so that
when there is a reduction in fluid pressure in the outlet port 77, as would be caused
by the opening of a valve in the hydraulic system (not shown) supplied by the outlet
port 77, the shiftable reaction member 95 rotates in the clockwise direction as viewed
in Figure 11 from the position shown in phantom toward the original position. This
movement of the shiftable reaction member 95 causes the variator to rotate from the
minimum flow position toward the maximum flow position.
[0044] Movement of the shiftable reaction member 95 is also opposed by the frictional force
resisting rotation of the outer rotor 21 within the variator 17. In some applications,
the frictional force applied by the cylindrical surface 54 to the eccentric inner
surface 19 will be sufficient to bias the variator toward the maximum flow position.
The frictional drag between the outer rotor 21 and the variator 17 combined with the
action of the spring 96 tends to shift the pump to maximum displacement when the pump
is started in the disclosed embodiment. Maximum flow at start up is desirable so that
the hydraulic system will be quickly pressurized to the proper operating pressure.
[0045] It should be understood that the extent to which the shiftable reaction member 95
shifts is dependent upon the degree of change in pressure in the outlet port 77. The
maximum flow position is established by a ball stop 97 which engages the second lobe
46 of the variator 17 to prevent movement past the maximum flow position which would
permit cross flow of fluid from the arcuate outlet groove 48 to the arcuate inlet
groove 49.
[0046] It should be understood that a conventional hydraulic control system can be used
to hydraulically control the displacement of the pump by simply connecting a hydraulic
line to a control fluid port 98 that is not open to the cylindrical bore 72. In such
a system injection or withdrawal of hydraulic fluid from the annular groove 92 could
be controlled from a remote location to selectively increase or decrease the displacement
of the pump.
OPERATION
[0047] Operation of the manually controlled variable displacement pump will be described
with reference to Figures 1 through 4. The displacement of the pump 10 is controlled
by shifting the handle 51 to move the pin 52 in the arcuate slot 53. The pin 52 in
turn shifts the variator 17 radially to rotate the eccentric axis "E" of the eccentric
bore 19 about the central axis "C". The second lobe 46 is simultaneously shifted toward
the first lobe 39 reducing the size of the annular outlet groove 49 and simultaneously
increasing the size of annular inlet groove 48. Shifting the eccentric axis "E" causes
the closed mesh area 62 of the inner and outer rotor to be rotated from the position
shown in Figure 3 toward the position shown in Figure 4.
[0048] In the minimum flow position shown in Figure 4, the fluid taken from the annular
inlet groove 48 is enclosed in the space 50 between adjacent teeth of the inner rotor
and outer rotor as they move across the first lobe 39. This action is commonly referred
to as (open mesh) crossover and it is at this zone that any fluid that has been drawn
into the space between the inner and outer rotors 22 and 21 is transferred from the
inlet groove 48 to the outlet groove 49. It should be noted that the space 50 between
the inner and outer rotors 22 and 21 adjacent the first lobe in the maximum flow position,
as shown in Figure 4, is several times larger than the space 50 adjacent the first
lobe in the minimum flow position, as shown in Figure 3, consequently, the amount
of displacement per revolution may be radically changed.
[0049] Operation of the automatically adjusted variable displacement pump 70 will next be
described with reference to Figures 11 and 12. The operation of the variable gerotor
pumping mechanism is identical to that described in the manual embodiment and will
not be described further because the shifting of the variator 82 results in the same
inneraction between the gerotor and the inlet and outlet ports.
[0050] With that in mind, shifting the automatically adjusting variable displacement pump
will be described. For illustration purposes, the system will be described as starting
in its maximum flow position as shown in solid lines in Figure 11. In this position,
similar to that shown in Figure 4, the maximum amount of fluid is transferred by the
gerotor.
[0051] If the demand for fluid is reduced, such as by the closing of a hydraulic valve downstream
from the outlet port 77, the pressure within the outlet port and between the inner
and outer rotors and in the control fluid port 98 will increase. The increase in pressure
is transferred to the annular groove 92 and is exerted on the shiftable reaction member
95 to overcome the resistance of the biasing member 96. The shiftable reaction member
95 is then moved in the counterclockwise direction, as shown in Figure 11, from the
position shown in solid lines to the position shown in phantom lines. By shifting
the shiftable reaction member 95 the variator is shifted to a reduced flow position.
[0052] If a demand is then placed on the outlet by the opening of a valve to a hydraulic
device such as a cylinder, the pressure in the outlet port 77, and between the inner
and outer rotors will likewise be reduced. This reduction in pressure is communicated
to the annular groove 92 through the control fluid port 98. When the pressure within
the annular groove 92 is reduced the shiftable reaction member 95 will be reacted
on by the spring 96 in the clockwise direction to rotate the variator 82 toward an
increased flow position. If the demand on the system is great enough, the variator
will shift to the maximum flow position wherein the second lobe moves to the position
diametrically opposed to the first lobe, until it contacts the ball stop 97.
[0053] It should be understood that the above description is to be taken by way of example
and not by way of limitation and that the present invention should be interpreted
in accordance with the following claims.
1. Rotary fluid power transmission unit having a housing (12) with a cylindrical bore
(13), a fluid intake (26) and a fluid outlet (27) communicating with said bore, and
having furthermore a fluid power transmisstion mechanism (20) with an outer power
transmission member (21) rotatably mounted within said housing (12) and an inner power
transmission member (22) nested within said outer power transmission member and eccentric
thereto and engaging said outer power transmission member, characterized by a positionable
control device (17) comprising a cylindrical body having an outer diameter rotatably
and adjustably nested in said bore (13) and having an inner diameter eccentric to
said outer diamter, said outer power transmission member (21) being rotatably nested
within said cylindrical body, the eccentric position between said outer power transmission
member (21) and said inner power transmission member (22) being variable for selectively
increasing and decreasing the effective power transmission volume of fluid by selective
rotation of said positionable control device (17) within said housing (12) and relative
to said outer and inner power transmission members (21, 22).
2. Power transmission unit in accordance with claim 1, characterized in that said
fluid power transmission mechanism (20) has the shape of a pump mechanism, said outer
power transmission member (21) being a controlled member and said inner power transmission
member (22) being a power driven control member drivingly engaging said controlled
member.
3. Power transmission unit in accordance with claim 2, characterized in that said
pump mechanism (20) is a gerotor pump mechanism, said controlled member being an outer
gerotor (21) having an outer cylindrical surface adapted to nest within the inner
cylindrical surface of the positionable control device (17) and an inner surface defining
a plurality of arcuate gear teeth, whereas said control member (22) has the shape
of an inner gerotor having an outer surface defining a plurality of arguate gear teeth
and being secured to a drive shaft (15).
4. Power transmission unit in accordance with one of the claims 1 to 3, characterized
in that said positionable control device (17) is adapted for infinitely positionable
angular relationship relative to said housing bore for correspondigly varying the
relative eccentric angular position of said outer and inner power transmission members
(21, 22) for a corresponding range between minimum and maximum fluid flow.
5. Power transmission unit in accordance with one of the claims 1 to 4, characterized
in that said cylindrical-body (82) of said positionable control device has a rotatable
fluid reaction member (95), that furthermore a stationary reaction member (93) is
provided on said housing (71) spaced from said rotatable fluid reaction member defining
a pressure chamber (92) and that channel means (98) are provided within said housing
(71) opening into said pressure chamber for delivering pressure fluid thereto, tending
to rotate said cylindrical body in one direction.
6. Power transmission unit in accordance with claim 5, charactrized in that opposing
spring means (96) are provided interposed between said housing (71) and said cylindrical
body (82) yieldably biasing said cylindrical body for rotation in the opposite direction
for creating a balance force condition depending upon an output volume demand connected
to said fluid outlet.
7. Power transmission unit in accordance with cairn 5 or 6, characterized in that
said cylindrical body (82) has an annular groove at its outer cylindrical surface,
said stationary reaction member (93) being nested within said groove, said movable
reaction member (95) being provided within said groove and movable relative to said
stationary reaction member.
8. Power transmission unit in accordance with claim 7, characterized in that said
spring means (96) include a coiled spring nested in said annular groove and being
anchored at one end to said housing (71) and at its other end to said cylindrical
body (82)
9. Power transmission unit in accordance with claim 8, characterized in that said
pressure chamber is defined by the inner cylindrical surface of said bore of said
housing (71) and the walls of said annular groove between said movable reaction member
which is secured to said cylindrical body (82) within said annular groove and being
in slidable sealing contact with said inner cylindrical surface of said bore, on the
one side, and said stationary reaction member (83) being firmly coupled to said housing
and,being in slidable sealing contact with the walls of said annular groove, on the
other side.
10. Power transmission unit in accordance with one of the claims 5 to 9, characterized
in that said channel means (98) interconnect said fluid outlet and said pressure chamber
for delivering pressure thereto tending to rotate said cylindircal body against spring
bias.
11. Power transmission unit in accordance with one of the claims 5 to 9, characterized
in that said channels means connect a variable pressure fluid source to said pressure
chamber for drivably pressurising said pressure chamber and thereby variably rotating
said cylindrical body against spring bias.
12. Power transmission unit in accordance with one of the claims 1 to 4, characterized
in that said positionable controlled device (17) is connected to a handle (51) through
an arcate slot (53) formed in a cover plate (24) which is removably secured to one
end of said housing (12).
13. Power transmission unit in accordance with one of the claims 1 to 12, characterized
in that said housing (12) has a port plate (14) said fluid intake (26) and said fluid
outlet (27) opening into said bore of said housing at said port plate (14), a commutator
(16) being provided having an annular portion with a first crossover element_(39)
extending radially outwardly from said annular portion, said commutator being secured
to said port plate (14) with the first crossover element (39) being located between
the fluid inlet port of the port plate on one side und the fluid outlet port of the
port plate on an opposite side, said positionable control device (17) having a second
crossover element (46) extending radially inwardly from a first inner surface of said
positionable control device which first inner surface is concentric relative to said
bore of said housing, a second inner surface of said positionable control device being
axially adjacent the first inner surface and being eccentric relative to said bore
of said housing with the central axis of the second inner surface being offset from
the central axis of said bore away from the second crossover element, said first crossover
element (39) engaging the first inner surface of said positionable control device
and the second crossover element (46) engaging the annular portion of the commutator
(16) to separate the fluid inlet and outlet ports.
14. Power transmission unit in accordance with claim 13, characterizied in that said
fluid inlet port is larger than said fluid outlet port.
15. Power transmission unit in accordance with claim 13 or 14, characterized in that
said commutator (16) is secured to said port plate (14) of said housing (12), both
crossover elements having the shape of radial lobes and:with the first crossover element
being fixedly located betwen the fluid inlet port and the fluid outlet port.
16. Power transmission unit in accordance with claim 15, characterized in that said
positionable control device (17) is adjustable by control means so that said second
crossover element is shifted from a maximum flow position wherein the second crossover
element is located diametrically opposite the first crossover element to a minimum
flow position wherein the second crossover element is immediately adjacent the opposite
side of the fluid outlet port from the first crossover element.